NXAJOY
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Aeromexico | Operator | on 2012-09-05 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
6 reports on file, 2021-05-31 – 2023-07-28.
Part: PACKING — LEAKING (ZONE 400) · airframe 59,243 hrs · 22,898 cycles
ENG NO 2 LOW ENG OIL INDICATION. FRM 790 070 52
Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 57,941 hrs · 22,367 cycles
AILERON DOES NOT GO BACK TO NEUTRAL LEFT & RIGHT FRM 271 060 48
Part: ANTI-SKID VALVE — ABNORMAL · airframe 55,156 hrs · 21,294 cycles
ENCIENDE LUZ DE ANTI-SKID DESPUES DE DESPEGUE, VALVULA ANTI-SKID SISTEMA DE FRENOS / ANTI-SKID LIGHT TURNS ON AFTER TAKEOFF, ANTI-SKID VALVE BRAKE SYSTEM
Part: NONE — LEAKING (ZONE 400) · airframe 54,250 hrs · 20,933 cycles
RIGHT ENGINE IDG PAD DRAIN WITH OIL LEAK. DURING TRANSIT CHECK, IT WAS A DETECTED AN OIL LEAK ON RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED A REVISION AT RIGHT ENGINE, DETECTING AN OIL LEAK ON IDG PAD DRAIN OF 20 DROPS PER MINUTE; SO THE SEALOL SEAL ASSEMBLY WAS REPLACED IAW AMM 72-63-00, TESTED CORRECT.
Part: ENGINE — DAMAGED (LEFT) · airframe 53,401 hrs · 20,559 cycles
26.07.2021 01:39 AIRCRAFT DURING CLIMB HAD LEFT ENGINE SHUTDOWN, AIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE LEFT ENGINE SHUTDOWN. MAINTENANCE PERSONNEL PERFORMED REVISION TO LEFT ENGINE CHIP DETECTOR, DETECTING METAL PARTICLE WASTE AND DURING PRELIMINARY INSPECTION FOUND INTERNAL DAMAGES OUT OF LIMITS; SO THE LEFT ENGINE P/N CFM56-7B27-3B1 WITH S/N 894756, TSN 51077, CSN 19555, MANUFACTURER CFM INTERNATIONAL, INC WAS REPLACED IAW MM 71-00-02-000-801 AND OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-00, TESTED CORRECT.
Part: DOOR — BULGED (APU) · airframe 52,886 hrs · 20,335 cycles
01.06.2021 17:11 A BULGE IN RIGHT COUNTER FRAME APU ACCESS DOOR. DURING TRANSIT CHECK, IT WAS DETECTED A BULGE IN FUSELAGE SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A BULGE OF 1.395" LENGTH, 0.156" WIDTH AND 0.010" DEPTH AT FUSELAGE SKIN SECTION 48 RH AT STA 1098.5 AT COUNTER FRAME APU DOOR; APU COWL DOOR WAS REMOVED IAW AMM 52-48-21-000-801; HFEC ISPECTION ON BULGE WAS PERFORMED IAW B737 NDTM PART 6, 51-00-00, PROCEDURES 16 AND 23, 53-30-00, PROCEDURE 3, NO CRACKS FOUND ON SKIN, FASTENER HOLE AND COUNTERSINK; FASTENER WAS INSTALLED IAW SRM 51-40-02, PARAGRAPH 4B; DAMAGE WAS REMOVED IAW SRM 53-80-01-2R-1, REPAIR 1, PARAGRAPH 4.B AND MESSAGE BOEING NUMBER AMX-AMX-21-0236-02B; HFEC INSPECTION ON BULGE WAS PERFORMED IAW B737 NDTM PART 6, 51-00-00, PROCEDURES 23; THE PERMANENT REPAIR WAS PERFORMED IAW SRM B737-53-80-01, REPAIR 1; THE APU COWL DOOR WAS INSTALLED IAW AMM 52-48-21-400-801, ALL CORRECT.